Item Details

Dynamic Response of a Mach 2.5 Axisymmetric Inlet and Turbojet Engine With a Poppet-Valve-Controlled Inlet-Stability Bypass System When Subjected to Internal and External Airflow Transients

Bobby W. Sanders
Format
EBook; Book; Government Document; Online
Published
Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1531
Description
1 online resource (iii, 98 pages) : illustrations.
Notes
  • Title from title screen (viewed Sept. 22, 2014).
  • "January 1980."
  • "Performing organization, Lewis Research Center"--Technical report documentation page.
  • Includes bibliographical references (pages 27-28).
Series Statement
NASA technical paper ; 1531
NASA technical paper 1531
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
  • Access in Virgo Classic

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    a| Airplanes x| Turbojet engines x| Air intakes.
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    a| Airplanes x| Motors x| Valves.
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